Orbital Test Vehicle

A United Launch Alliance (ULA) Atlas V rocket successfully launched the Air Force Space Command 5 (AFSPC-5) satellite for the U.S. Air Force at 11:05 a.m. EDT on May 20, 2015 from Space Launch Complex-41. The rocket carried the X-37B Orbital Test Vehicle or OTV, a reliable, reusable, unmanned space test platform for the U.S. Air Force.

A United Launch Alliance (ULA) Atlas V rocket successfully launched the AFSPC-5 satellite for the U.S. Air Force from Space Launch Complex-41. This is ULA’s fifth launch in 2015 and the 96th successful launch since the company was formed in December 2006

«ULA is honored to launch this unique spacecraft for the U.S Air Force. Congratulations to the Air Force and all of our mission partners on today’s successful launch! The seamless integration between the Air Force, Boeing, and the entire mission team culminated in today’s successful launch of the Atlas V AFSPC-5 mission», said Jim Sponnick, ULA vice president, Atlas and Delta Programs.

This Atlas V mission also includes the Aft Bulkhead Carrier (ABC) carrying the National Reconnaissance Office’s (NRO’s) Ultra Lightweight Technology and Research Auxiliary Satellite (ULTRASat). ULTRASat is composed of 10 CubeSats managed by the NRO and NASA. «The ABC contained 8 P-Pods that released 10 CubeSats that were successfully delivered. The CubeSats were developed by the U.S Naval Academy, the Aerospace Corporation, Air Force Research Laboratory, The Planetary Society and California Polytechnic, San Luis Obispo to conduct various on orbit experiments», said Sponnick.

This mission was launched aboard an Atlas V 501 configuration Evolved Expendable Launch Vehicle (EELV), which includes a 5.4-meter-diameter payload fairing. The Atlas booster for this mission was powered by the RD AMROSS RD-180 engine, and the Centaur upper stage was powered by the Aerojet Rocketdyne RL10C-1 engine. This was ULA’s sixth launch of the 501 configuration, and ULA’s 54th mission to launch on an Atlas V rocket.

ULA’s next launch is the Atlas V GPS IIF-10 mission for the U. S. Air Force, scheduled for July 15 from Space Launch Complex-41 from Cape Canaveral Air Force Station, Florida.

The EELV program was established by the United States Air Force to provide assured access to space for Department of Defense and other government payloads. The commercially developed EELV program supports the full range of government mission requirements, while delivering on schedule and providing significant cost savings over the heritage launch systems.

With more than a century of combined heritage, United Launch Alliance is the nation’s most experienced and reliable launch service provider. ULA has successfully delivered more than 90 satellites to orbit that provide critical capabilities for troops in the field, aid meteorologists in tracking severe weather, enable personal device-based GPS navigation and unlock the mysteries of our solar system.

ULA has successfully delivered more than 90 satellites to orbit that provide critical capabilities for troops in the fi eld, aid meteorologists in tracking severe weather, enable personal device-based GPS navigation and unlock the mysteries of our solar system

X-37B

The X-37B Orbital Test Vehicle, or OTV, is an experimental test program to demonstrate technologies for a reliable, reusable, unmanned space test platform for the U.S. Air Force. The primary objectives of the X-37B are twofold: reusable spacecraft technologies for America’s future in space and operating experiments, which can be returned to, and examined, on Earth.

The X-37B Orbital Test Vehicle is the newest and most advanced re-entry spacecraft. Based on NASA’s X-37 design, the unmanned OTV is designed for vertical launch to Low Earth Orbit (LEO) altitudes where it can perform long duration space technology experimentation and testing. Upon command from the ground, the OTV autonomously re-enters the atmosphere, descends and lands horizontally on a runway. The X-37B is the first vehicle since NASA’s shuttle orbiter with the ability to return experiments to Earth for further inspection and analysis, however the X-37B can stay in space for much longer.

The Atlas V vehicle will also launch an Aft Bulkhead Carrier (ABC) containing eight P-Pods will release 10 CubeSats. Following primary spacecraft separation the Centaur will change altitude and inclination in order to release the CubeSat spacecraft, which are sponsored by the National Reconnaissance Office (NRO) and the National Aeronautics and Space Administration (NASA). The ten CubeSats were developed by the U.S. Naval Academy, the Aerospace Corporation, the Air Force Research Laboratory, California Polytechnic State University, and Planetary Society.

Payload Fairing (PLF)

The AFSPC-5 satellite is encapsulated in a 5-m (14-feet) diameter medium payload fairing. The 5-m PLF is a sandwich composite structure made with a vented aluminum-honeycomb core and graphite-epoxy face sheets. The bisector (two-piece shell) PLF encapsulates both the Centaur and the satellite. The vehicle’s height with the 5-m medium PLF is approximately 63 m/206 feet.

In preparation for launch, an Atlas V rocket, with the Air Force’s AFSPC-5 mission, is rolled from the Vertical Integration Facility or VIF to the pad at Space Launch Complex-41

Centaur

The Centaur second stage is 3 m/10 feet in diameter and 12.65 m/41.5 feet in length. Its propellant tanks are constructed of pressure-stabilized, corrosion resistant stainless steel. Centaur is a cryogenic vehicle, fueled with liquid hydrogen and liquid oxygen. It uses a single RL10C-1 engine producing 101.86 kN/10,387 kg/22,900 lbs of thrust. The cryogenic tanks are insulated with a combination of helium-purged insulation blankets, radiation shields, and Spray-On Foam Insulation (SOFI). The Centaur forward adapter (CFA) provides the structural mountings for the fault-tolerant avionics system and the structural and electrical interfaces with the spacecraft.

With more than a century of combined heritage, United Launch Alliance is the nation’s most experienced and reliable launch service provider

Booster

The Atlas V booster is 3.8 m/12.5 feet in diameter and 32.46 m/106.5 feet in length. The booster’s tanks are structurally rigid and constructed of isogrid aluminum barrels, spun-formed aluminum domes, and intertank skirts. Atlas booster propulsion is provided by the RD-180 engine system (a single engine with two thrust chambers). The RD-180 burns RP-1 (Rocket Propellant-1 or highly purified kerosene) and liquid oxygen, and delivers 3,826.36 kN/390,180 kg/860,200 lbs of thrust at sea level. The Atlas V booster is controlled by the Centaur avionics system, which provides guidance, flight control, and vehicle sequencing functions during the booster and Centaur phases of flight.